Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:burnTime |
150 s
|
| gptkbp:chamberPressure |
4.8 MPa
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:cycle |
gas-generator cycle
|
| gptkbp:diameter |
0.89 m
|
| gptkbp:firstFlight |
1956
|
| gptkbp:fuelType |
gptkb:RP-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
LR79 rocket engine
|
| gptkbp:length |
3.05 m
|
| gptkbp:manufacturer |
gptkb:North_American_Aviation
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:specificImpulseVacuum |
247 s
285 s |
| gptkbp:status |
retired
|
| gptkbp:thrustSeaLevel |
607 kN
|
| gptkbp:thrustVacuum |
670 kN
|
| gptkbp:usedFor |
ballistic missiles
space launch vehicles |
| gptkbp:usedIn |
gptkb:satellite
gptkb:Atlas_missile gptkb:Jupiter_missile gptkb:Thor_missile |
| gptkbp:weight |
725 kg
|
| gptkbp:bfsParent |
gptkb:Rocketdyne
|
| gptkbp:bfsLayer |
6
|